1.北京航空航天大学 能源与动力工程学院,北京 100191
2.北京航空航天大学 航空发动机结构强度北京市重点实验室,北京 100191
李琳(1956-),女,教授、博士生导师,博士,主要从事航空发动机结构振动分析及抑制等研究。
吴亚光(1990-),男,博士后,主要从事非线性与智能结构动力学研究。E⁃mail:yaguangwu@buaa.edu.cn
移动端阅览
李琳, 高钱, 吴亚光, 等. 考虑参数关联的缘板阻尼器减振性能分析[J]. 航空动力学报, 2021,36(8):1657-1668.
Lin LI, Qian GAO, Yaguang WU, et al. On the vibration reduction performance of underplatform dampers considering parameter correlation[J]. Journal of Aerospace Power, 2021, 36(8): 1657-1668.
李琳, 高钱, 吴亚光, 等. 考虑参数关联的缘板阻尼器减振性能分析[J]. 航空动力学报, 2021,36(8):1657-1668. DOI: 10.13224/j.cnki.jasp.20200373.
Lin LI, Qian GAO, Yaguang WU, et al. On the vibration reduction performance of underplatform dampers considering parameter correlation[J]. Journal of Aerospace Power, 2021, 36(8): 1657-1668. DOI: 10.13224/j.cnki.jasp.20200373.
建立了缘板阻尼器(UPDs)各参数间的关联关系,揭示了减振性能随主要参数的变化规律,形成参数联动设计准则。基于双叶片⁃缘板阻尼器集中参数模型,采用多阶谐波平衡法(MHBM)计算稳态响应以衡量阻尼器性能;推导了解析雅可比矩阵,使收敛性和计算效率显著提高。结果表明:考虑参数的关联性是必要的;选取较大材料密度与特定底角的对称楔形缘板阻尼器,可以实现4.57%的最优阻尼比;当激振力存在相位差时,采用非对称的楔形阻尼结构能进一步提升阻尼效果。
The correlation between principal parameters of wedge underplatform dampers (UPDs) was established to reveal the influence of these relevant parameters on the damping effect,and then to summarize the design guidelines considering parameter correlation.Based on the lumped parameter model of a two blades⁃UPD system which can describe the motion containing phase lag between blades,the steady state response of the system was simulated by the multi⁃harmonic balance method (MHBM),and the reduction of the resonance amplitude was used to quantify the damping performance.In order to improve the convergence and efficiency of the algorithm,the Jacobian matrix was deduced analytically.Results showed that it was necessary to consider the parameter correlation.The damper performance of wedge UPDs can be optimized to 4.57% by choosing larger material density and appropriate wedge angles.Asymmetric wedge dampers can further improve the damping effect under excitation with phase lag.
陈璐璐 , 马艳红 , 杨鑫 . 带干摩擦阻尼结构叶片振动响应试验 [J]. 航空动力学报 , 2008 , 23 ( 9 ): 1647 ⁃ 1653 .
CHEN Lulu , MA Yanhong , YANG Xin . Blade vibration with dry friction damping [J]. Journal of Aerospace Power , 2008 , 23 ( 9 ): 1647 ⁃ 1653 . (in Chinese)
李琳 , 刘久周 , 李超 . 航空发动机中的干摩擦阻尼器及其设计技术研究进展 [J]. 航空动力学报 , 2016 , 31 ( 10 ): 2305 ⁃ 2317 .
LI Lin , LIU Jiuzhou , LI Chao . Research progress of dry friction damper and its design technology in aeroengine [J]. Journal of Aerospace Power , 2016 , 31 ( 10 ): 2305 ⁃ 2317 . (in Chinese)
MENQ C H , GRIFFIN J H , BIELAK J . The influence of a variable normal load on forced vibration of a frictional damped system [J]. Journal of Engineering for Gas Turbines and Power , 1986 , 108 ( 2 ): 300 ⁃ 305 .
何尚文 , 任兴民 , 秦卫阳 , 等 . 基于微滑移模型的B⁃G型叶片干摩擦缘板阻尼器减振特性研究 [J]. 振动与冲击 , 2012 , 31 ( 1 ): 44 ⁃ 48 .
HE Shangwen , REN Xingmin , QIN Weiyang , et al . Study on damping characteristics of B⁃G dry friction damper based on micro slip model [J]. Vibration and Shock , 2012 , 31 ( 1 ): 44 ⁃ 48 . (in Chinese)
GRIFFIN J H . Friction damping of resonant stresses in gas turbine engine airfoils [J]. Journal of Engineering for Power , 1998 , 102 ( 2 ): 329 ⁃ 333 .
SIEWERT C , PANNING L , WALLASCHEK J , et al . Multiharmonic forced response analysis of a turbine blading coupled by nonlinear contact forces [J]. Journal of Engineering for Gas Turbines and Power , 2010 , 132 ( 8 ): 287 ⁃ 296 .
GOLA M M , GASTALDI C . Understanding complexities in underplatform damper mechanics [R]. ASME Paper GT2014⁃25240 , 2014 .
PETROV E P , EWINS D J . Advanced modeling of underplatform friction dampers for analysis of blades disk vibration [J]. Journal of Turbomachinery , 2007 . 129 ( 1 ): 143 ⁃ 150 .
PETROV E P . A high⁃accuracy model reduction for analysis of nonlinear vibrations in structures with contact interfaces [J]. Journal of Engineering for Gas Turbines and Power , 2011 , 133 ( 10 ): 102503.1 ⁃ 102503.10 .
李琳 , 刘久周 , 李超 . 干摩擦阻尼器对宽频多阶次激励减振效果分析 [J]. 航空动力学报 , 2016 , 31 ( 9 ): 2171 ⁃ 2180 .
LI Lin , LIU Jiuzhou , LI Chao . Analysis of damping effect of dry friction damper on broadband multi order excitation [J]. Journal of Aeronautical Dynamics , 2016 , 31 ( 9 ): 2171 ⁃ 2180 . (in Chinese)
YANG B D , MENQ C H . Characterization of contact kinematics and application to the design of wedge dampers in turbomachinery blading:Part 1 stick⁃slip contact kinematics [J]. Journal of Engineering for Gas Turbines and Power , 1998 , 120 ( 2 ): 410 ⁃ 417 .
PFEIFER F , HAJEK M . Stick⁃slip motion of turbine blade dampers [J]. Philosophical Transactions of the Royal Society:Physical and Engineering Sciences , 1992 , 338 : 503 ⁃ 517 .
FIRRONE C M , ZUCCA S . Modelling friction contacts in structural dynamics and its application to turbine bladed disks [M]. Berlin , Germany:InTech , 2011 .
PANNING L , SEXTRO W , POPP K . Optimization of interblade friction damper design [R]. ASME Paper 2000⁃GT⁃0541 , 2000 .
GOLA M M , SANTOS M B D , LIU T . Measurement of the scatter of underplatform damper hysteresis cycle:experimental approach [R]. Chicago,USA : ASME International Design Engineering Technical Conferences and Computers and Information in Engineering Conference , 2012 .
FIRRONE C M , ZUCCA S , GOLA M M . The effect of underplatform dampers on the forced response of bladed disks by a coupled static/dynamic harmonic balance method [J]. International Journal of Nonlinear Mechanics , 2011 , 46 ( 2 ): 363 ⁃ 375 .
POUDOU O J . Modeling and analysis of the dynamics of dry⁃friction⁃damped structural systems [D]. Michigan , USA:The University of Michigan , 2007 .
马皓晔 , 李琳 , 范雨 , 等 . 基于加速动态拉格朗日法的摩擦片阻尼分析 [J]. 航空学报 , 2019 , 40 ( 12 ): 121 ⁃ 133 .
MA Haoye , LI Lin , FAN Yu , et al . Analysis of friction plate damping based on accelerated dynamic Lagrangian method [J]. Acta Aeronautica et Astronautica Sinica , 2019 , 40 ( 12 ): 121 ⁃ 133 . (in Chinese)
FIRRONE C M . Measurement of the kinematics of two underplatform dampers with different geometry and comparison with unmerical simulation [J]. Journal of Sound and Vibration , 2009 , 323 ( 1 ): 323 ⁃ 333 .
郝燕平 , 单颖春 , 朱梓根 . 缘板摩擦阻尼器的减振实验研究 [J]. 航空动力学报 , 2001 , 16 ( 1 ): 55 ⁃ 58 .
HAO Yanping , SHAN Yingchun , ZHU Zigen . Experimental study on vibration reduction of edge plate friction damper [J]. Journal of Aerospace Power , 2001 , 16 ( 1 ): 55 ⁃ 58 . (in Chinese)
ZUCCA S , BOTTO D . Range of variability in dynamics of semi⁃cylindrical friction dampers for turbine blades [R]. ASME Paper GT2008⁃51058 , 2008 .
ZHANG Dayi , GAO Bin . Experimental inverstigation on dynamic response of falt blades with underplatform dampers [J]. Chinese Journal of Aeronautics , 2019 , 32 ( 12 ): 2667 ⁃ 2678 .
单颖春 , 朱梓根 , 刘献栋 . 带缘板摩擦阻尼器叶片的非线性振动响应研究 [J]. 振动、测试与诊断 , 2006 , 26 ( 2 ): 126 ⁃ 132 .
SHAN Yingchun , ZHU Zigen , LIU Xiandong . Study on nonlinear vibration response of blade with friction damper [J]. Vibration ,Test and Diagnosis, 2006 , 26 ( 2 ): 126 ⁃ 132 . (in Chinese)
SANLITURK K Y , EWINS D J . Underplatform dampers for turbine blades:theoretical modeling,analysis,and compariosn with experimental data [J]. Journal of Engineering for Gas Turbines and Power , 2001 , 123 ( 4 ): 327 ⁃ 338 .
阳刚 , 周标 , 臧朝平 , 等 . 缘板阻尼结构减振特性的影响因素分析 [J]. 航空动力学报 , 2019 , 34 ( 1 ): 115 ⁃ 124 .
YANG Gang , ZHOU Biao , ZANG Chaoping , et al . Analysis of influence factors on vibration reduction characteristics of edge plate damping structure [J]. Journal of Aerospace Power , 2019 , 34 ( 1 ): 115 ⁃ 124 . (in Chinese)
GASTALDI C , GOLA M M . Criteria for best performance of pre⁃optimized solid dampers [J]. Journal of Engineering for Gas Turbines and Power , 2019 , 141 ( 4 ): 042502.1 ⁃ 042502.9 .
YANG B D , MENQ C H . Characterization of contact kinematics and application to the design of wedge dampers in turbomachinery blading:Part 2 prediction of forced response and experimental verification [J]. Journal of Engineering for Gas Turbines and Power , 1998 , 120 ( 2 ): 418 ⁃ 423 .
0
浏览量
1
下载量
0
CSCD
关联资源
相关文章
相关作者
相关机构
京公网安备11010602201714号